Stall Delay and Leading-Edge Suction for a Pitching Airfoil with Trailing-Edge Flap-Reference-Cited by-同舟云学术

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Stall Delay and Leading-Edge Suction for a Pitching Airfoil with Trailing-Edge Flap

Published:2020-12 Issue:12 Volume:58 Page:5146-5155
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

He Guosheng,Deparday Julien,Siegel Lars,Henning Arne,Mulleners Karen¹

Affiliation:

1. Federal Institute of Technology Lausanne, CH-1015 Lausanne, Switzerland

Funder

Schweizerischer Nationalfonds zur Förderung der Wissenschaftlichen Forschung

Deutsche Forschungsgemeinschaft

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference32 articles.

1. Progress in analysis and prediction of dynamic stall

2. Controlled leading-edge suction for management of unsteady separation over pitching airfoils

3. Suppression of dynamic-stall vortices over pitching airfoils by leading-edge suction

4. Control of dynamic flowfield around a pitching NACA633−618 airfoil by a DBD plasma actuator

5. Dynamic Stall Control around Practical Airfoil Using Nanosecond-Pulse-Driven Dielectric Barrier Discharge Plasma Actuators

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1. Nonlinear-Model-Inversion Control for Stall-Flutter Suppression of an Airfoil via Camber Morphing;AIAA Journal;2024-08-13

2. Data-driven transient lift attenuation for extreme vortex gust–airfoil interactions;Journal of Fluid Mechanics;2024-08-10

3. Machine-Learning-Enhanced Real-Time Aerodynamic Forces Prediction Based on Sparse Pressure Sensor Inputs;AIAA Journal;2024-07

4. Fast Aerodynamic Prediction of Airfoil with Trailing Edge Flap Based on Multi-Task Deep Learning;Aerospace;2024-05-09

5. Research of Unsteady Aerodynamic Characteristics of Electrically Controlled Rotor Airfoils with Trailing-Edge Flaps;Aerospace;2023-12-24

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